View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 85U 61004C 23024.14599419 .00011082 00000-0 20961-2 0 9999
2 85 38.7639 186.8082 0360634 26.2903 335.5673 14.29935023 66617
| Epoch (UTC): | 24 January 2023 03:30:13 |
| Eccentricity: | 0.0360634 |
| inclination: | 38.7639° |
| perigee height: | 533 km |
| apogee height: | 1050 km |
| right ascension of ascending node: | 186.8082° |
| argument of perigee: | 26.2903° |
| revolutions per day: | 14.29935023 |
| mean anomaly at epoch: | 335.5673° |
| orbit number at epoch: | 6661 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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